Structural polymeric laminates, quartz textiles and white thermal control coatings were evaluated for design of typical orbital vehicle; selection of materials was predicated upon their capability to exhibit greatest degree of dimensional and functional stability when subjected to long term exposure in orbital environment; desired characteristics of these materials are outlined. (31863)
Long life materials for spacecraft
Soc Aerospace Matl Process Engrs Nat Symp
13th SAMPE National Symposium -- Energistic Materials -- Energy to Benefit of Aerospace and Mankind ; 1968 Materials
1968
32 pages
Conference paper
English
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